Accuracy Improvement of the Spacecraft Attitude Determination by the ESG/FOG Data Fusion
Spacecraft Attitude Determination Using Electrostatically Suspended Gyros
The Use of Angular Rate Multiple Integrals as Input Signals for Strapdown Attitude Algorithms
Use of Specific Force Multiple Integrals as Input Signals for Strapdown Navigation Algorithms
An Attitude Reference System with Solid-Rotor ESGs for Orbital Satellites